Damage tolerance of continuous fibre composites: Material and environmental effects

被引：5

作者：

Bibo, GA ^{[1
]}

Hogg, PJ ^{[1
]}

机构：

[1] Queen Mary Univ London, Dept Mat, London E1 4NS, England

来源：

IMPACT RESPONSE AND DYNAMIC FAILURE OF COMPOSITES AND LAMINATE MATERIALS, PTS 1 AND 2 | 1998年 / 141-1卷

关键词：

textiles; compression after impact; environmental conditioning;

D O I：

10.4028/www.scientific.net/KEM.141-143.93

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Aerospace design philosophies are used to discuss critically, the suitability of composite materials to primary structural applications. The principal issues limiting the use of composites, compression after impact performance and high cost, are examined in terms of material/manufacturing form and environmental conditioning. The material types investigated consist of thermoset and thermoplastic matrix reinforced unidirectional prepreg tape and textile manufactured architectures.

引用

页码：93 / 126

页数：34

共 140 条

[1]

[Anonymous], 37 INT SAMPE S 9 12

[2]

BABIC L, 1989, PLAST RUB PROC APPL, V12, P199

[3]

BACKHOUSE R, 1996, 20 C INT COUNC AER S, V1, P950

[4] STRONG BENDING IN THE DCB INTERLAMINAR TEST OF THIN, E-GLASS WOVEN-FABRIC-REINFORCED LAMINATES [J].

BAZHENOV, SL .

COMPOSITES, 1991, 22 (04) :275-280

[5]

BERGSTROM DF, 1992, 37 INT SAMPE S EXH C, V32, P278

[6] HIGH-TEMPERATURE DAMAGE TOLERANCE OF CARBON-FIBER-REINFORCED PLASTICS .1. IMPACT CHARACTERISTICS [J].

BIBO, G ;

LEICY, D ;

HOGG, PJ ;

KEMP, M .

COMPOSITES, 1994, 25 (06) :414-424

[7] HIGH-TEMPERATURE DAMAGE TOLERANCE OF CARBON-FIBER-REINFORCED PLASTICS .2. POSTIMPACT COMPRESSION CHARACTERISTICS [J].

BIBO, GA ;

HOGG, PJ ;

KEMP, M .

COMPOSITES, 1995, 26 (02) :91-102

[8]

BIBO GA, 1997, ICCM 11 AUSTR

[9]

BIBO GA, 1997, IN PRESS J COMPOSITE

[10]

BIBO GA, 1995, 3 INT C DEF FRACT CO, P374

← 1 2 3 4 5 6 7 8 9 10 →